# STC SA02262SE - Type: Supplemental type certificate - Status: Current, Issued - Holder: Stene Aviation Inc, United States - Description: Installation of split seam wing strut cuff as replacement parts for the strut fairings - Applied: March 25, 2012 - Status date: March 8, 2013 - Product: Aircraft, Small Airplane - Certification basis: Part 21 - Data sheets: [TCDS 3A19](https://openairdocs.org/tcds/3A19), [TCDS 3A12](https://openairdocs.org/tcds/3A12), [TCDS 3A17](https://openairdocs.org/tcds/3A17), [TCDS 5A6](https://openairdocs.org/tcds/5A6), [TCDS 3A13](https://openairdocs.org/tcds/3A13), [TCDS 3A24](https://openairdocs.org/tcds/3A24), [TCDS A4CE](https://openairdocs.org/tcds/A4CE), [TCDS 3A21](https://openairdocs.org/tcds/3A21) - Certificate PDF: https://openairdocs.org/files/sha256/08/06/0806791bbce78f0611f986e8f9825df592e6964c63fba5bc2751bfe6ee3014e8 - Approved model list and other attachments: [AML_SA02262SE.pdf](https://openairdocs.org/files/sha256/9f/cc/9fccb38c854ae108e80198149f0c812ebe517d30295249bfecb875d36c9d376e) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/589D9DE9353ECB3186257B2C004D6A0B.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA02262SE ## ADs that name it (0) None. ## Approved models (106, first 50) - Cessna Aircraft Company 150 ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 150A ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 150B ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 150C ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 150D ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 150E ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 150F ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 150G ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 150H ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 150J ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 150K ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 150L ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 150M ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 152 ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 172 ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172A ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172B ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172C ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172D ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172E ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172F (USAF T-41A) ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172G ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172H (USAF T-41A) ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172I ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172K ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172L ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172M ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172N ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172P ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172Q ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172R ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172RG ([TCDS 3A17](https://openairdocs.org/tcds/3A17)) - Cessna Aircraft Company 172S ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 175 ([TCDS 3A17](https://openairdocs.org/tcds/3A17)) - Cessna Aircraft Company 175A ([TCDS 3A17](https://openairdocs.org/tcds/3A17)) - Cessna Aircraft Company 175B ([TCDS 3A17](https://openairdocs.org/tcds/3A17)) - Cessna Aircraft Company 175C ([TCDS 3A17](https://openairdocs.org/tcds/3A17)) - Cessna Aircraft Company 180 ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180A ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180B ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180C ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180D ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180E ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180F ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180G ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180H ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180J ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180K ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182A ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) All 106: https://openairdocs.org/stc/SA02262SE/models.md ## What the certificate says Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record. United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Number SA02262SE This certificate, issued to Stene Aviation Inc. 470 Regatta Rd. P.O. Box 700 Polson, MT 59860 Part * of the * Regulations. Original ProductType Certificate Number: * See attached Federal Aviation Administration (FAA) Make: Approved Model List (AML) SA02262SE for approved Model: aircraft models and applicable airworthiness regulations Description of the Type Design Change: Installation of split seam wing strut cuff as replacement parts for the strut fairings in accordance with Stene Aviation Inc. Part Drawing Eligibility Table SA700PDET, Revision IR, dated March 6, 2013, or later FAA approved revision. Fabrication is controlled by Stene Aviation part numbers given in Report SA700STRUT-1 dated April 11, 2012, or later FAA-approved revision. Maintained in accordance with Stene Aviation “Instructions for Continued Airworthiness,” Document Number SA700_ICA, Revision A, or later FAA-accepted revision. Limitations and Conditions: Approval of this change in type design applies to the aircraft listed on AML SA02262SE only. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the relationship between this change and other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this certificate, the AML, and ICA must be maintained as part of the permanent records for the modified aircraft. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. Date of application: March 25, 2012 Date reissued: Date of issuance: March 8, 2013 Date amended: (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) ### AML_SA02262SE.pdf **FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA02262SE FOR** INSTALLATION OF A SPLIT SEAM WING STRUT CUFF ISSUE DATE: March 8, 2013 Page 1 of 1 **ITEM AIRCRAFT MAKE** **AIRCRAFT MODEL ORIGINAL TC NUMBER** **CERTIFICATION** **BASIS FOR** **ALTERATION** **FAA APPROVED PART** **DRAWING ELIGIBILITY TABLE** AML REV DATE Document Revision* 1. Cessna 150, 150A, 150B, 150C, 150D, 150E, 150F, 150G, 150H, 150J, 150K, 150L, 150M, 152 3A19 CAR 3 SA700PDET Revision A, dated March 6, 2013 2. Cessna 172, 172A, 172B, 172C, 172D, 172E, 172F, 172G, 172H, 172I, 172K, 172L, 172M, 172N, 172P, 172Q, 172R, 172S 3A12 CAR 3 SA700PDET Revision A, dated March 6, 2013 3. Cessna 175, 175A, 175B, 175C, 175RG, R172K, P172D 3A17 CAR 3 SA700P DET Revision A, dated March 6, 2013 4. Cessna 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, 182R, T182, 182S, R182, TR182 3A13 CAR 3 SA700PDET Revision A, dated March 6, 2013 5. Cessna 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J, 180K 5A6 CAR 3 SA700PDET Revision A, dated March 6, 2013 6. Cessna 205, 205A 3A21 CA R 3 SA700PDET Revision A, dated March 6, 2013 7. Cessna 206, P206, P 206A, TP206A, P206B, TP206B, P206C, TP206C, P206D, TP206D, 206E, TP206E, U206, U206A, TU206A, U206B, TU206B, U206C, TU206C, U206D, TU206D, U206E, TU206E, U206F, TU206F A4CE CAR 3 SA700PDET Revision A, dated March 6, 2013 8. Cessna 185, 185A, 185B, 185C, 185D, 185E, A185E, A185F 3A24 CAR 3 SA700PDET Revision A, dated March 6, 2013 * Or later FAA Approved Revision FAA Approved: Acting Manager, Seattle Aircraft Certification Office AMENDED: REISSUED: ## Every issue (1) - March 8, 2013: Issued, Current. [certificate](https://openairdocs.org/files/sha256/08/06/0806791bbce78f0611f986e8f9825df592e6964c63fba5bc2751bfe6ee3014e8), [AML_SA02262SE.pdf](https://openairdocs.org/files/sha256/9f/cc/9fccb38c854ae108e80198149f0c812ebe517d30295249bfecb875d36c9d376e) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.